1. Field of the Invention
This invention relates to vessel propulsion systems, and in particular to a modular hydraulic thruster system for vessel.
2. Background of the Invention
Marine thrusters typically mount on barges and flat boats, and are used as propulsion for these vessels. One type of marine thruster employs a prime mover such as a diesel engine driving a hydraulic pump, together known as a “power pack”, and the resultant pressurized hydraulic fluid may be employed to drive a propeller attached to a lower unit.
A number of designs exist for this type of flat boat propulsion system, with attendant problems. One problem is the lack of readily available instrumentation to depict important condition information such as the angle of thrust at which a given thruster is aiming relative to the centerline of the vessel to which it is attached, the power output being developed in terms of propeller revolutions per minute, the tilt angle of the thruster lower unit, the degree of extension or retraction of the thruster lower unit, and the condition of any clamps in the system (open or closed).
Another problem with existing marine thruster designs is the absence of a quick and easy means to add additional thrusters to the system, as required. It would be desirable to provide a modular hydraulic thruster system for vessel which provides the provisions for readily attaching additional thrusters as required for a flat vessel whose weight loading and/or thruster requirements may be changing.
It would also be desirable to provide a modular hydraulic thruster system for vessel which comprises indication capability including displays of the angle of thrust at which a given thruster is aiming relative to the centerline of the vessel to which it is attached, the power output being developed in terms of propeller revolutions per minute, the tilt angle of the thruster lower unit, the degree of extension or retraction of the thruster lower unit, and the condition of any clamps in the system (open or closed).
Accordingly, it is an object of the present invention to provide a modular hydraulic thruster system for vessel which provides thrust angle information to the pilot. Design features allowing this object to be accomplished include thrust angle detection means to detect a thrust angle of the propeller electrically connected to a thruster angle indicator in an instrument panel. Advantages associated with the accomplishment of this object include increased safety and efficiency of operation.
It is another object of the present invention to provide a modular hydraulic thruster system for vessel which advises the open/closed status of thruster tube gear clamp(s). Design features allowing this object to be accomplished include tube gear clamp OPEN/CLOSED status indication means electrically connected to a tube gear clamp status indicator in an instrument panel. Benefits associated with the accomplishment of this object include greater facility of operation and aid in eliminating errors when extending and retracting the thruster tube.
It is still another object of this invention to provide a modular hydraulic thruster system for vessel which provides effective protection to tube gear clamp hydraulic lines and tube gear clamp wire. Design features enabling the accomplishment of this object include a swivel union whose swivel union rotating section is attached to a tube, and whose swivel union stationary section is prevented from rotating relative to a thruster housing, and flexible spiral conduit slidably encircling the tube from the swivel union to the tube gear clamp. Advantages associated with the realization of this object include the ability to protect tube gear clamp hydraulic and electrical lines, while extending and retracting the tube relative to the housing.
It is another object of the present invention to provide a modular hydraulic thruster system for vessel which provides thrust power information to the pilot. Design features allowing this object to be accomplished include revolutions per minute detection means at a hydraulic motor electrically connected to a tachometer in an instrument panel. Benefits associated with the accomplishment of this object is more precise thruster control, and attendant efficiency of operation increase.
It is still another object of this invention to provide a modular hydraulic thruster system for vessel which provides un-interrupted hydraulic and electric lines continuity to a tube gear clamp and tube lower end, even while changing the angle between the housing and the tube during steering. Design features enabling the accomplishment of this object include a swivel union whose swivel union rotating section is attached to a tube; whose swivel union stationary section is prevented from rotating relative to a thruster housing; close clamp hydraulic line, open clamp hydraulic line, forward thrust hydraulic line, reverse thrust hydraulic line, return hydraulic line, tube gear clamp wire, and tachometer wire passing through the swivel union. Advantages associated with the realization of this object include conversion of hydraulic and electrical lines from stationary to rotating, and the consequent ability to steer the thruster through a 360 degree arc.
It is another object of the present invention to provide a modular hydraulic thruster system for vessel which provides thruster tilt angle to the pilot. Design features allowing this object to be accomplished include angle-of-tilt detection means connected to a tilt actuator, and a tilt angle indicator in an instrument panel. Benefits associated with the accomplishment of this object is more precise operation of a vessel upon which the modular hydraulic thruster system for vessel, with attendant efficiency and safety increases.
It is still another object of this invention to provide a modular hydraulic thruster system for vessel which provides thruster extension information to the pilot. Design features enabling the accomplishment of this, object include a percentage-of-extension detection means connected to an extension actuator, and an extension indicator in an instrument panel. Benefits associated with the accomplishment of this object is more precise operation of a vessel upon which the modular hydraulic thruster system for vessel, with attendant efficiency and safety increases.
It is yet another object of this invention to provide a modular hydraulic thruster system for vessel which is economical to produce. Design features allowing this object to be achieved include the use of commercially available elements, and components made of readily available materials. Benefits associated with reaching this objective include reduced cost, and hence increased availability.
The invention, together with the other objects, features, aspects and advantages thereof will be more clearly understood from the following in conjunction with the accompanying drawings.
Five sheets of drawings are provided. Sheet one contains
Power pack 80 comprises prime mover 82, pump 84, and reservoir 86. In the preferred embodiment, prime mover 82 was a diesel or internal combustion engine, pump 84 was a hydraulic pump driven by prime mover 82, and reservoir 86 contained hydraulic fluid pumped by pump 84, as driven by prime mover 82.
Instrument panel 60 contains instrumentation to continuously communicate information and status including displays of the angle of thrust at which a given thruster 4 is aiming relative to the centerline of the vessel to which it is attached, the power output being developed in terms of propeller revolutions per minute, the tilt angle of the thruster lower unit, the degree of extension or retraction of the thruster tube 6, and the condition of any clamps in the system (open or closed). The instant apparatus associated with these functions will be explained more fully below.
One or more thrusters 4 may be connected to instrument panel 60 and power pack 80, depending on the thruster power requirements of a specific vessel. In the preferred embodiment, thrusters 4 were hydraulic thrusters, and each thruster 4 was hydraulically connected with power pack 80, and electrically connected to instrument panel 60.
Housing 35 is rotatably attached to bracket 8 at pivot points 37. In use, bracket 8 is rigidly attached to a vessel, and serves as the attachment point for thruster 4 to a vessel upon which thruster 4 is mounted. Stop 34 is rigidly attached to, and extends downwards from, bracket 8. Stop 34 butts up against the stern of the vessel, and provides a positive mechanical stop for thruster 4 to exert forward force against the vessel.
At least one tilt actuator arm 28 extends upwards from housing 35. One end of tilt actuator 26 is rotatably attached to an end of an associated tilt actuator arm 28; an opposite end of tilt actuator 26 is rotatably attached to an end of bracket 8 opposite housing 36. Retraction and extension of tilt actuator 26 causes housing 35 to rotate upwards around pivot points 37, and downwards around pivot points 37, respectively.
Tube 6 is sized to slidably fit into cylinder bore 33 in cylinder 32. Thus, tube 6 is free to rotate and reciprocate within cylinder 32. Referring now also to
Tube gear clamp 36 contains tube gear clamp bore 38, which is sized to slidably admit tube 6. Tube gear clamp key 40 extends into tube gear clamp bore 38, and is sized to slidably reciprocate within tube keyway 44 in tube 6. Tube gear clamp key 40 reciprocating within tube keyway 44 prevents tube 6 from rotating relative to tube gear clamp 36 and tube gear 24. Thus, when steering motor 20 turns tube gear 24 and rigidly attached tube gear clamp 36, tube 6 turns at the same rate, thus providing a steering function to thruster 4.
Tube gear clamp 36 further comprises tube gear clamp actuator 42, which loosens and tightens tube gear clamp 36 on tube 6. Tube gear clamp 36 must be loosened, or opened, prior to extending or retracting tube 6 within cylinder 32, and tube gear clamp actuator 42 permits opening and closing of tube gear clamp 26 to be accomplished remotely.
Given that tube gear clamp 36 must be opened prior to extending or retracting tube 6 within cylinder 32, and closed thereafter, it is important to provide a tube gear clamp 36 condition indication (OPEN or CLOSED) at instrument panel 60, as explained below.
Following extension or retraction of tube 6, tube gear clamp 36 must be closed or tightened, in order to prevent tube 6 from rotating within tube gear clamp 36 while steering.
Thruster 4 also has at least one extension actuator 30 which permits tube 6 to be extended and retracted relative to cylinder 32. Extension actuator 30 is attached at its lower end to cylinder 32, and at its upper end to collar 14. Collar 14 has collar bore 15 sized to slidably admit tube 6.
Swivel union 12 having an upper swivel union stationary section 46 rotatably attached to a lower swivel union rotating section 48 is disposed atop tube 6. Swivel union rotating section 48 is attached to the top of tube 6, and rotates with tube 6. Swivel union stationary section 46 is prevented from rotating by means of anti-rotation member 16, an upper end of which is rigidly attached to swivel union stationary section 46. Swivel union 12 includes electronic angle detection means to determine and transmit to instrument panel 60 via electrical signal the angle between swivel union stationary section 46 and swivel union rotating section 48.
Anti-rotation member 16 is maintained in constant vertical orientation relative to housing 35 by means of antirotation member guide(s) 18 rigidly attached to housing 35. Each anti-rotation guide 18 is sized to slidably admit anti-rotation member 16. In the preferred embodiment, one anti-rotation member guide 18 was rigidly attached at an upper edge of housing 35, and another anti-rotation member guide 18 was rigidly attached at a lower edge of housing 35.
Because anti-rotation member 16 is free to reciprocate within anti-rotation member guides 18 (which are rigidly attached to housing 36), and because an upper end of anti-rotation guide 16 is rigidly attached to swivel union stationary section 46, swivel union 12 is free to rise as urged by collar 15 actuated by extension actuator(s) 30 (while simultaneously being prevented from rotating relative to housing 35 by anti-rotation member 16); and is also free to descend with collar 15 under the influence of gravity when extension actuator(s) 30 are retracted (while simultaneously being prevented from rotating relative to housing 36 by anti-rotation member 16).
Thus, tube 6 is retracted by extension of extension actuator(s) 30, which pushes both collar 15 and swivel union 12 upwards. Tube 6 is extended by retraction of extension actuator(s) 30, which permits both collar 15 and swivel union 12 to descend under the influence of gravity.
In the preferred embodiment, propeller 10 turns as urged by reversible hydraulic motor 108 at the bottom end of tube 6. Referring to
Tube gear clamp 36 opens and closes under hydraulic fluid pressure. When tube gear clamp 36 is commanded to open, hydraulic fluid travels under pressure from pump 84, through open clamp valve 92 (close clamp valve 90 remains closed), and via open clamp hydraulic line 93 to tube gear clamp 36. Similarly, when tube gear clamp 36 is commanded to close, hydraulic fluid travels under pressure from pump 84, through close clamp valve 90 (open clamp valve 92 remains closed), and via close clamp hydraulic line 91 to tube gear clamp 36.
Tube 6 tilts up and down under hydraulic fluid pressure to tilt actuator 26. When tilt actuator 26 is commanded to retract, thereby tilting tube 6 up, hydraulic fluid travels under pressure from pump 84, through tilt up valve 100 (tilt down valve 102 remains closed), and via tilt up hydraulic line 101 to tilt actuator 26. Similarly, when tilt actuator 26 is commanded to extend, thereby tilting tube 6 down, hydraulic fluid travels under pressure from pump 84, through tilt down valve 102 (tilt down valve 100 remains closed), and via tilt down hydraulic line 103 to tilt actuator 26.
Tube 6 extends and retracts under hydraulic fluid pressure to extension actuator 30. When extension actuator 30 is commanded to extend, thereby retracting tube 6, hydraulic fluid travels under pressure from pump 84, through extension valve 104 (retraction valve 106 remains closed), and via extension hydraulic line 105 to extension actuator 30. Similarly, when extension actuator 30 is commanded to retract, thereby extending tube 6, hydraulic fluid travels under pressure from pump 84, through retraction valve 106 (extension valve 104 remains closed), and via retraction hydraulic line 107 to extension actuator 30.
Referring now also to
Thrust angle indicator 66 indicates the angle of thrust of propeller 10 relative to the centerline of a vessel upon which modular hydraulic thruster system for vessel 2 is mounted. Swivel union 12 includes electronic angle detection means to determine and transmit to instrument panel 60 via electrical signal the angle between swivel union stationary section 46 and swivel union rotating section 48.
Thruster angle wire 73 carries the resultant electric signal from the swivel union 12 electronic angle detection means to thruster angle indicator 66, whose needle indicates the angle between swivel union stationary section 46 and swivel union rotating section 48, calibrated to indicate zero degrees when the thrust from propeller 10 is aimed directly backwards, aligned with the centerline of the vessel. In
Tube gear clamp status indicator 64 indicates whether tube gear clamp 36 is opened or closed. This is important information to have readily available, because as explained above, tube gear clamp 36 must be opened prior to extending or retracting tube 6 within cylinder 32, and closed thereafter. Tube gear clamp 36 includes electronic OPEN/CLOSED status indication means to determine and transmit to instrument panel 10 via electrical signal whether tube gear clamp 36 is opened or closed.
Tube gear clamp wire 74 carries the resultant electrical signal from the tube gear clamp 36 electronic OPEN/CLOSED status indication means to tube gear clamp status indicator 64 in instrument panel 60. Tube gear clamp status indicator 64 then displays the status, e.g. with a light illuminating under indicia, LED display, LCD display, etc.
As may be observed in
An additional complication exits relative to the hydraulic and electrical lines running from swivel union rotating section 48 to tube gear clamp 36. Because tube 6 reciprocates within cylinder 32 as tube 6 extends and retracts, the distance between swivel union rotating section 48 and tube gear clamp 36 may vary considerably. It is therefore necessary to employ a variable-length conduit to carry the hydraulic and electrical lines running from swivel union rotating section 48 to tube gear clamp 36.
The instant design runs close clamp hydraulic line 91, open clamp hydraulic line 93, and tube gear clamp wire 74 through flexible spiral conduit 17 between swivel union rotating section 48 to tube gear clamp 36. Flexible spiral conduit 17 is wrapped several turns around tube 6, and due to its flexibility and spiral shape, can accommodate the full extension/retraction travel of tube 6.
Because close clamp hydraulic line 91, open clamp hydraulic line 93, and tube gear clamp wire 74 are connected to swivel union stationary section 46 inside tube 6, tube aperture 7 sized to admit these permits their egress from the inside of tube 6, and into flexible spiral conduit 17 to tube gear clamp 36. Thus, close clamp hydraulic line 91, open clamp hydraulic line 93, and tube gear clamp wire 74 run from swivel union stationary section 46, through tube aperture 7, through flexible spiral conduit 17, and to tube gear clamp 36.
Extension indicator 68 indicates the percentage extension of tube 6 relative to housing 36. This indication is important, because in brackish or other low-visibility water, the degree of extension of tube 6 cannot be ascertained visually. Extension actuator 30 includes electronic percentage-of-extension detection means to determine and transmit to instrument panel 10 via electrical signal the extent of extension of extension actuator 30. Extension wire 72 carries the resultant electrical signal from the extension actuator 30 electronic percentage-of-extension detection means from extension actuator 30 to extension indicator 68 in instrument panel 60. Extension indicator 68 shows the percentage extension of tube 6 relative to housing 35, and is indicated as being 75% extended in
Tilt angle indicator 70 indicates the tilt angle of tube 6. This indication is important, because the operator of modular hydraulic thruster system for vessel 2 may be facing forward, and thruster(s) 4 behind such operator may not be readily visible. Tilt actuator 26 includes electronic angle-of-tilt detection means to determine and transmit to instrument panel 60 via electrical signal the extent of extension of tilt actuator 30, which is proportional to the tilt angle of tube 6. Tilt angle wire 71 carries the resultant electrical signal from the tilt actuator 26 electronic angle-of-tilt detection means from tilt actuator 26 to tilt angle indicator 70 in instrument panel 60. Tilt angle indicator 70 shows the angle tilt of tube 6, and is indicated as being thirty degrees up from completely down in
Tachometer 62 indicates the rotation speed of propeller 10, typically displayed in revolutions per minute. This indication is important, because revolutions per minute of propeller 10 represents the amount of thrust power being developed at propeller 10. Electronic revolutions per minute detection means (such as a rotating magnet on the shaft of propeller 10 and an associated stationary sensor) is disposed in the proximity of hydraulic motor 108 to determine and transmit to instrument panel 10 via electrical signal the speed of propeller 10. Tachometer wire 75 carries the resultant electrical signal from the electronic revolutions per minute detection means to tachometer 62 in instrument panel 60. In
Instrument panel 60 may include thrust angle indicator 66, tube gear clamp status indicator 64, extension indicator 68, tilt angle indicator 70, and tachometer 62 as discrete instruments, as parts of a unified display such as a liquid crystal display or monitor, or any other appropriate display means.
In the preferred embodiment, the structural components of thruster 4 and reservoir 86 were made of metal, synthetic, or other appropriate material. Steering motor 56; swivel union 12; collar 14; tube gear 24; steering motor gear 20; tube gear clamp 36; tilt actuator 26; extension actuator 20; hydraulic motor 108; propeller 10; valves 20, 92, 94, 96, 102, 104, 106 and 108; the hydraulic lines; the electrical lines; flexible spiral conduit 17; extension actuator 30 electronic percentage-of-extension detection means; tilt actuator 26 includes electronic angle-of-tilt detection means; electronic revolutions per minute detection means; and hydraulic power pack 22 were commercially available items.
Instrument panel 60 may include thrust angle indicator 66, tube gear clamp status indicator 64, extension indicator 68, tilt angle indicator 70, and tachometer 62 as discrete instruments, as parts of a unified display such as a liquid crystal display or monitor, or any other appropriate display means.
In the preferred embodiment, tilt actuator 26 and extension actuator 30 were hydraulic actuators powered by pressurized hydraulic fluid from hydraulic power pack 80, although it is intended to fall within the scope of this disclosure that these elements be any appropriate actuator, including but not limited to electrical actuators, solenoids, linear motors, rack-and-pinion gear arrangements, etc. Similarly, in the preferred embodiment steering motor 20 was a hydraulic motor, but it is intended to fall within the scope of this disclosure that this elements be any appropriate motor, including electrical, etc.
While a preferred embodiment of the invention has been illustrated herein, it is to be understood that changes and variations may be made by those skilled in the art without departing from the spirit of the appending claims.
This utility patent application is a Continuation-In-Part of U.S. application Ser. No. 12/381,245 filed Mar. 10, 2009 entitled now U.S. Pat. No. 7,883,384 Self-Contained Hydraulic Thruster for Vessel, which is a Continuation-In-Part of U.S. application Ser. No. 11/999,531 filed Dec. 6, 2007 now U.S. Pat. No. 7,654,875 entitled Self-Contained Hydraulic Thruster for Vessel, which was based upon U.S. provisional patent application Ser. No. 60/903,400 filed Feb. 26, 2007 entitled Modular Hydraulic Thruster System for Vessel; and claims the benefit of the earlier filing date of these applications.
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Number | Date | Country | |
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60903400 | Feb 2007 | US |
Number | Date | Country | |
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Parent | 12381245 | Mar 2009 | US |
Child | 12800026 | US | |
Parent | 11999531 | Dec 2007 | US |
Child | 12381245 | US |